GB1470036A - Dual range sound absorber - Google Patents
Dual range sound absorberInfo
- Publication number
- GB1470036A GB1470036A GB217375A GB217375A GB1470036A GB 1470036 A GB1470036 A GB 1470036A GB 217375 A GB217375 A GB 217375A GB 217375 A GB217375 A GB 217375A GB 1470036 A GB1470036 A GB 1470036A
- Authority
- GB
- United Kingdom
- Prior art keywords
- horn
- sheet
- array
- core
- horns
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10K—SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- G10K11/00—Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/16—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
- G10K11/172—Methods or devices for protecting against, or for damping, noise or other acoustic waves in general using resonance effects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/10—Properties of the layers or laminate having particular acoustical properties
- B32B2307/102—Insulating
Abstract
1470036 Sound absorbing laminate LOCKHEED AIRCRAFT CORP 17 Jan 1975 2174/75 Heading B5N [Also in Divisions G5 and H3] A wide range sound absorber comprises an impermeable backing sheet 1, a core of orthogonally intersecting portions 2, 3, an array 4 of tapered horns 5, and may have a permeable facing sheet 11, all of which are bonded together, e.g. by an adhesive. The mouths of the horns 5 may be circular, square or rectangular and may be above, flush with or below the top of said core. The narrow throat of the horn in the embodiment of Fig. 1 is spaced from the backing sheet 1 but in other embodiments said throat contacts the sheet 1 and an aperture is provided in the horn (Figs. 3, 4, not shown). The array 4 is preferably made from vacuumformed plastics, and the facing sheet 11 from fibre metal, perforated metal, porous paper, porous ceramic or other suitable material having a flow resistance of the order of 1 pc (p and c respectively being the density of and velocity of sound in the propagating fluid medium). The shape of the horn may be exponential, hyperbolic, catenoidal, Bessel or conical.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB217375A GB1470036A (en) | 1975-01-17 | 1975-01-17 | Dual range sound absorber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB217375A GB1470036A (en) | 1975-01-17 | 1975-01-17 | Dual range sound absorber |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1470036A true GB1470036A (en) | 1977-04-14 |
Family
ID=9734870
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB217375A Expired GB1470036A (en) | 1975-01-17 | 1975-01-17 | Dual range sound absorber |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1470036A (en) |
Cited By (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2300081A (en) * | 1995-04-20 | 1996-10-23 | Dornier Gmbh | Acoustic absorber |
US5760349A (en) * | 1995-04-20 | 1998-06-02 | Dornier Gmbh | Acoustic absorber having a slotted horn arranged in a pot |
GB2341742A (en) * | 1998-09-21 | 2000-03-22 | Blast Loudspeakers Limited | An acoustic absorber or emitter |
WO2005091272A1 (en) * | 2004-03-17 | 2005-09-29 | Eads Deutschland Gmbh | Assembly for reducing noise in turbofan engines |
WO2011082510A1 (en) * | 2010-01-08 | 2011-07-14 | 中国科学院声学研究所 | Compound sound absorption device with built-in resonant cavity |
WO2015023389A1 (en) * | 2013-08-12 | 2015-02-19 | Hexcel Corporation | Sound wave guide for use in acoustic structures |
EP2846030A1 (en) * | 2013-08-30 | 2015-03-11 | Airbus Defence and Space GmbH | Sound absorber, sound absorber assembly and an engine with a sound absorber assembly |
WO2015026421A3 (en) * | 2013-07-29 | 2015-04-09 | The Boeing Company | Septumization of honeycomb sandwiches |
KR20160043057A (en) * | 2013-08-12 | 2016-04-20 | 헥셀 코포레이션 | Noise absorbing structure comprising a honeycomb with an internal septum |
EP2605238A3 (en) * | 2011-12-13 | 2016-11-02 | Rolls-Royce Deutschland Ltd & Co KG | Acoustic absorber |
CN107610688A (en) * | 2017-09-05 | 2018-01-19 | 上海声望声学科技股份有限公司 | A kind of compound sound insulating structure of lumen |
FR3055662A1 (en) * | 2017-04-24 | 2018-03-09 | Airbus Operations (S.A.S.) | INTERNAL STRUCTURE OF A PRIMARY EJECTION DUCT OF A TURBOMACHINE COMPRISING AN ABSORBENT STRUCTURE OF LOW FREQUENCY SOUNDS |
CN109147750A (en) * | 2018-11-15 | 2019-01-04 | 中车株洲电力机车有限公司 | A kind of low frequency coupling sound absorption structure |
FR3078431A1 (en) * | 2018-02-28 | 2019-08-30 | Airbus Operations | SOUNDPROOFING COATING COMPRISING AN ALVEOLAR STRUCTURE WITH CURVED CELLS SHAPED ON EITHER OF THE SAME INTERNAL WALL |
BE1026313B1 (en) * | 2018-07-20 | 2019-12-23 | Houtbuigerij G Desmet Nv | SOUND-ABSORBABLE PANEL AND METHOD FOR MANUFACTURING SUCH SOUND-Absorbing PANEL |
CN111099010A (en) * | 2017-08-29 | 2020-05-05 | Mra***有限责任公司 | Acoustic liner, method of forming the same, and aircraft engine assembly having the acoustic liner |
CN111354329A (en) * | 2018-12-24 | 2020-06-30 | 空中客车运营简化股份公司 | Method for manufacturing a sound-absorbing structure comprising a honeycomb panel with integrated acoustic elements and sound-absorbing structure obtained by this method |
EP3696090A1 (en) * | 2019-02-14 | 2020-08-19 | Airbus Operations (S.A.S.) | Method for manufacturing an acoustic absorption structure including a skin forming a plurality of enclosures, acoustic absorption structure obtained according to said method and aircraft comprising said acoustic absorption structure |
WO2020174192A1 (en) * | 2019-02-28 | 2020-09-03 | Safran Nacelles | Method for creating alveolar cores having open inner conical shapes |
FR3099963A1 (en) * | 2019-08-13 | 2021-02-19 | Airbus Operations | Acoustic element with double enclosure and reduced bulk, in particular for aircraft acoustic panels |
WO2021176182A1 (en) * | 2020-03-04 | 2021-09-10 | Safran Nacelles | Method for manufacturing a structure with cellular cores for a turbojet nacelle |
-
1975
- 1975-01-17 GB GB217375A patent/GB1470036A/en not_active Expired
Cited By (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2300081A (en) * | 1995-04-20 | 1996-10-23 | Dornier Gmbh | Acoustic absorber |
US5760349A (en) * | 1995-04-20 | 1998-06-02 | Dornier Gmbh | Acoustic absorber having a slotted horn arranged in a pot |
GB2300081B (en) * | 1995-04-20 | 1998-11-18 | Dornier Gmbh | Acoustic absorber |
GB2341742A (en) * | 1998-09-21 | 2000-03-22 | Blast Loudspeakers Limited | An acoustic absorber or emitter |
GB2341742B (en) * | 1998-09-21 | 2003-04-23 | Blast Loudspeakers Ltd | Acoustic absorber and emitter |
WO2005091272A1 (en) * | 2004-03-17 | 2005-09-29 | Eads Deutschland Gmbh | Assembly for reducing noise in turbofan engines |
JP2007529666A (en) * | 2004-03-17 | 2007-10-25 | エーアーデーエス・ドイッチェランド・ゲゼルシャフト ミット ベシュレンクテル ハフツング | Noise reduction structure in turbofan engine |
US7819224B2 (en) | 2004-03-17 | 2010-10-26 | Eads Deutschland Gmbh | Assembly for reducing noise in turbofan engines |
JP4659021B2 (en) * | 2004-03-17 | 2011-03-30 | エーアーデーエス・ドイッチェランド・ゲゼルシャフト ミット ベシュレンクテル ハフツング | Noise reduction structure in turbofan engine |
WO2011082510A1 (en) * | 2010-01-08 | 2011-07-14 | 中国科学院声学研究所 | Compound sound absorption device with built-in resonant cavity |
EP2605238A3 (en) * | 2011-12-13 | 2016-11-02 | Rolls-Royce Deutschland Ltd & Co KG | Acoustic absorber |
US10363726B2 (en) | 2013-07-29 | 2019-07-30 | The Boeing Company | Septumization of honeycomb sandwiches |
WO2015026421A3 (en) * | 2013-07-29 | 2015-04-09 | The Boeing Company | Septumization of honeycomb sandwiches |
US9643392B2 (en) | 2013-07-29 | 2017-05-09 | The Boeing Company | Septumization of honeycomb sandwiches |
CN105493176A (en) * | 2013-08-12 | 2016-04-13 | 赫克赛尔公司 | Sound wave guide for use in acoustic structures |
KR20160043056A (en) * | 2013-08-12 | 2016-04-20 | 헥셀 코포레이션 | Sound wave guide for use in acoustic structures |
KR20160043057A (en) * | 2013-08-12 | 2016-04-20 | 헥셀 코포레이션 | Noise absorbing structure comprising a honeycomb with an internal septum |
JP2016532155A (en) * | 2013-08-12 | 2016-10-13 | ヘクセル コーポレイション | Sound waveguide for use in acoustic structures |
AU2014307026B2 (en) * | 2013-08-12 | 2017-04-20 | Hexcel Corporation | Sound wave guide for use in acoustic structures |
KR102228528B1 (en) | 2013-08-12 | 2021-03-15 | 헥셀 코포레이션 | Sound wave guide for use in acoustic structures |
WO2015023389A1 (en) * | 2013-08-12 | 2015-02-19 | Hexcel Corporation | Sound wave guide for use in acoustic structures |
KR102228530B1 (en) | 2013-08-12 | 2021-03-15 | 헥셀 코포레이션 | Noise absorbing structure comprising a honeycomb with an internal septum |
EP2846030A1 (en) * | 2013-08-30 | 2015-03-11 | Airbus Defence and Space GmbH | Sound absorber, sound absorber assembly and an engine with a sound absorber assembly |
US9303588B2 (en) | 2013-08-30 | 2016-04-05 | Airbus Defence and Space GmbH | Sound absorber, sound absorber assembly and an engine with a sound absorber assembly |
FR3055662A1 (en) * | 2017-04-24 | 2018-03-09 | Airbus Operations (S.A.S.) | INTERNAL STRUCTURE OF A PRIMARY EJECTION DUCT OF A TURBOMACHINE COMPRISING AN ABSORBENT STRUCTURE OF LOW FREQUENCY SOUNDS |
CN111099010A (en) * | 2017-08-29 | 2020-05-05 | Mra***有限责任公司 | Acoustic liner, method of forming the same, and aircraft engine assembly having the acoustic liner |
CN111099010B (en) * | 2017-08-29 | 2023-11-10 | Mra***有限责任公司 | Acoustic liner, method of forming the same, and aircraft engine assembly having the acoustic liner |
CN107610688B (en) * | 2017-09-05 | 2024-04-26 | 同济大学 | Cavity tube composite sound insulation structure |
CN107610688A (en) * | 2017-09-05 | 2018-01-19 | 上海声望声学科技股份有限公司 | A kind of compound sound insulating structure of lumen |
US11268478B2 (en) | 2018-02-28 | 2022-03-08 | Airbus Operations Sas | Sound-proofing covering comprising a cellular structure with curved cells formed on either side of one and the same inner wall |
EP3534360A1 (en) * | 2018-02-28 | 2019-09-04 | Airbus Operations S.A.S. | Soundproofing coating comprising a honeycomb structure with curved cells formed on either side of a single inner wall |
FR3078431A1 (en) * | 2018-02-28 | 2019-08-30 | Airbus Operations | SOUNDPROOFING COATING COMPRISING AN ALVEOLAR STRUCTURE WITH CURVED CELLS SHAPED ON EITHER OF THE SAME INTERNAL WALL |
BE1026313B1 (en) * | 2018-07-20 | 2019-12-23 | Houtbuigerij G Desmet Nv | SOUND-ABSORBABLE PANEL AND METHOD FOR MANUFACTURING SUCH SOUND-Absorbing PANEL |
CN109147750A (en) * | 2018-11-15 | 2019-01-04 | 中车株洲电力机车有限公司 | A kind of low frequency coupling sound absorption structure |
CN111354329A (en) * | 2018-12-24 | 2020-06-30 | 空中客车运营简化股份公司 | Method for manufacturing a sound-absorbing structure comprising a honeycomb panel with integrated acoustic elements and sound-absorbing structure obtained by this method |
EP3696090A1 (en) * | 2019-02-14 | 2020-08-19 | Airbus Operations (S.A.S.) | Method for manufacturing an acoustic absorption structure including a skin forming a plurality of enclosures, acoustic absorption structure obtained according to said method and aircraft comprising said acoustic absorption structure |
FR3092844A1 (en) * | 2019-02-14 | 2020-08-21 | Airbus Operations (S.A.S.) | A method of making an acoustic absorption structure comprising a skin forming a plurality of enclosures, an acoustic absorption structure obtained by said method and an aircraft comprising said acoustic absorption structure |
FR3093374A1 (en) * | 2019-02-28 | 2020-09-04 | Safran Nacelles | Process for the development of alveolar cores with open internal conical shapes |
CN113490978A (en) * | 2019-02-28 | 2021-10-08 | 赛峰短舱公司 | Method for manufacturing honeycomb core having open internal conical shape |
EP3931821A1 (en) * | 2019-02-28 | 2022-01-05 | Safran Nacelles | Method for creating alveolar cores having open inner conical shapes |
WO2020174192A1 (en) * | 2019-02-28 | 2020-09-03 | Safran Nacelles | Method for creating alveolar cores having open inner conical shapes |
FR3099963A1 (en) * | 2019-08-13 | 2021-02-19 | Airbus Operations | Acoustic element with double enclosure and reduced bulk, in particular for aircraft acoustic panels |
FR3107856A1 (en) * | 2020-03-04 | 2021-09-10 | Safran Nacelles | Manufacturing process of a honeycomb core structure for a turbojet nacelle |
WO2021176182A1 (en) * | 2020-03-04 | 2021-09-10 | Safran Nacelles | Method for manufacturing a structure with cellular cores for a turbojet nacelle |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |